首页 | 本学科首页   官方微博 | 高级检索  
     检索      

无人机绳钩回收系统的动力学特性仿真分析
引用本文:卢伟,马晓平,周明,孙林峰.无人机绳钩回收系统的动力学特性仿真分析[J].航空学报,2015,36(10):3295-3304.
作者姓名:卢伟  马晓平  周明  孙林峰
作者单位:西北工业大学 365所, 西安 710072
摘    要:无人机(UAV)精确定点回收是促进中小型无人机广泛应用的关键技术,而绳钩回收是一种适合小型固定翼无人机在狭窄场地或舰船上实现精确定点回收的先进回收方式,其具有良好的研究应用价值和开发前景。采用基于矢量封闭环、欧拉运动学和动力学方程的联立约束法,解决了无人机绳钩回收系统的空间机构运动的动力学求解问题。基于无人机绳钩回收系统动力学模型,对无人机回收时系统吸能缓冲过程中的动力学特性进行了深入分析。在MATLAB/Simulink环境中通过对动力学模型的仿真,得出以无人机速度变化为代表的系统主要性能指标,同时探讨了参数变化对系统主要性能的影响,并分析了回收过程中拦阻力峰值载荷下的机翼应力和应变。结果表明,无人机绳钩回收性能优良,是一种可开发研制的新型回收技术,为开展无人机绳钩回收系统的工程研制提供了重要的理论参考。

关 键 词:无人机  绳钩回收  吸能缓冲  动力学特性  仿真分析  
收稿时间:2014-10-20
修稿时间:2014-12-15

Simulation analysis of dynamic characteristic of UAV rope-hook recovery system
LU Wei,MA Xiaoping,ZHOU Ming,SUN Linfeng.Simulation analysis of dynamic characteristic of UAV rope-hook recovery system[J].Acta Aeronautica et Astronautica Sinica,2015,36(10):3295-3304.
Authors:LU Wei  MA Xiaoping  ZHOU Ming  SUN Linfeng
Institution:The 365th Institute, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:Accurate-point recovery of unmanned aerial vehicle (UAV) is a critical technology to promote the widespread use of small- and medium-sized UAVs. The rope-hook recovery technology provides an advanced accurate-point recovery method for small-sized fixed-wing UAV in limited recovery fields or naval vessels, which is of great value in advanced research and application and has splendid future. The space mechanism dynamics problem of the rope-hook recovery system is resolved by using the simultaneous constraint method based on the closing-vector-circle method and Euler kinematical and dynamical equations. The energy-absorbing and buffer capability of the rope-hook recovery system is deeply analyzed based on the dynamic modeling of UAV rope-hook recovery system. The main characteristic of the system, for instance, the velocity change, is estimated through the simulation of the dynamics modeling in the environment of MATLAB/Simulink. The influences of parameter variation on the system's main characteristics are discussed. The stress and strain of the wing forced by the arresting peak load in the process of recovery are analyzed. The results and analysis show preliminarily that the rope-hook recovery system has good performance and is a new recovery technology to develop. It offers a significant theoretical reference for the manufacture of the UAV rope-hook recovery system.
Keywords:UAV  rope-hook recovery  energy-absorbing and buffer  dynamic characteristic  simulation analysis  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号